JPWO2021186718A1 - - Google Patents

Info

Publication number
JPWO2021186718A1
JPWO2021186718A1 JP2022508003A JP2022508003A JPWO2021186718A1 JP WO2021186718 A1 JPWO2021186718 A1 JP WO2021186718A1 JP 2022508003 A JP2022508003 A JP 2022508003A JP 2022508003 A JP2022508003 A JP 2022508003A JP WO2021186718 A1 JPWO2021186718 A1 JP WO2021186718A1
Authority
JP
Japan
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2022508003A
Other languages
Japanese (ja)
Other versions
JP7210805B2 (en
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Publication of JPWO2021186718A1 publication Critical patent/JPWO2021186718A1/ja
Application granted granted Critical
Publication of JP7210805B2 publication Critical patent/JP7210805B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/08—Geodetic or other open-frame structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
JP2022508003A 2020-03-19 2020-03-19 Support and support mounting method Active JP7210805B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2020/012473 WO2021186718A1 (en) 2020-03-19 2020-03-19 Support body and support body mounting method

Publications (2)

Publication Number Publication Date
JPWO2021186718A1 true JPWO2021186718A1 (en) 2021-09-23
JP7210805B2 JP7210805B2 (en) 2023-01-23

Family

ID=77771072

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2022508003A Active JP7210805B2 (en) 2020-03-19 2020-03-19 Support and support mounting method

Country Status (4)

Country Link
US (1) US11840362B2 (en)
EP (1) EP4105003A4 (en)
JP (1) JP7210805B2 (en)
WO (1) WO2021186718A1 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001310798A (en) * 2000-04-27 2001-11-06 Honda Motor Co Ltd Method of manufacturing fuselage structure of fiber- reinforced composite material, and fuselage structure manufactured by the same
JP2006056022A (en) * 2004-08-17 2006-03-02 Murata Mach Ltd Manufacturing method of reinforcing fiber preform for curved frp beam material
WO2010140205A1 (en) * 2009-06-01 2010-12-09 三菱重工業株式会社 Method for manufacturing composite material member and laminated body of prepreg sheet
JP2013534478A (en) * 2010-06-25 2013-09-05 ザ・ボーイング・カンパニー Composite structure having integral stiffener and method for producing the same
JP2017052237A (en) * 2015-09-11 2017-03-16 三菱重工業株式会社 Manufacturing apparatus of fiber-reinforced plastic molded product and manufacturing method thereof

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR687024A (en) * 1928-12-20 1930-08-04 Emboutissage Et De Const Mecan Improvements made to hollow bodies forming hulls, in particular to aircraft fuselages
US3976269A (en) * 1974-12-19 1976-08-24 The Boeing Company Intrinsically tuned structural panel
US5560102A (en) * 1992-10-13 1996-10-01 The Boeing Company Panel and fuselage assembly
JP4425424B2 (en) * 2000-05-01 2010-03-03 本田技研工業株式会社 Method for producing semi-cured article with joggle made of fiber reinforced composite material, and method for producing preformed structure using the same
JP4522796B2 (en) 2004-09-06 2010-08-11 本田技研工業株式会社 Manufacturing method of fiber reinforced composite material annular structure and annular frame for aircraft fuselage comprising the structure
US9102103B2 (en) 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
DE102007021075B4 (en) * 2007-05-04 2012-06-28 Airbus Operations Gmbh Connecting arrangement for connecting two curved frames of an aircraft or spacecraft
FR2993856B1 (en) 2012-07-30 2015-09-18 Airbus Operations Sas AIRCRAFT FUSELAGE STRUCTURE ELEMENT HAVING AN EVOLVING SECTION
IL242749B (en) * 2015-11-24 2019-08-29 Israel Aerospace Ind Ltd Aircraft panel and method of constructing
DE102019111836B4 (en) * 2019-05-07 2023-06-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Profile component for reinforcing component structures, component structure and manufacturing process for this

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001310798A (en) * 2000-04-27 2001-11-06 Honda Motor Co Ltd Method of manufacturing fuselage structure of fiber- reinforced composite material, and fuselage structure manufactured by the same
JP2006056022A (en) * 2004-08-17 2006-03-02 Murata Mach Ltd Manufacturing method of reinforcing fiber preform for curved frp beam material
WO2010140205A1 (en) * 2009-06-01 2010-12-09 三菱重工業株式会社 Method for manufacturing composite material member and laminated body of prepreg sheet
JP2013534478A (en) * 2010-06-25 2013-09-05 ザ・ボーイング・カンパニー Composite structure having integral stiffener and method for producing the same
JP2017052237A (en) * 2015-09-11 2017-03-16 三菱重工業株式会社 Manufacturing apparatus of fiber-reinforced plastic molded product and manufacturing method thereof

Also Published As

Publication number Publication date
US11840362B2 (en) 2023-12-12
US20230140085A1 (en) 2023-05-04
EP4105003A1 (en) 2022-12-21
JP7210805B2 (en) 2023-01-23
EP4105003A4 (en) 2023-04-12
WO2021186718A1 (en) 2021-09-23

Similar Documents

Publication Publication Date Title
BR112023005462A2 (en)
BR112023012656A2 (en)
BR112021014123A2 (en)
BR112022009896A2 (en)
BR112022024743A2 (en)
BR112023009656A2 (en)
BR112023006729A2 (en)
BR102021015500A2 (en)
BR102021007058A2 (en)
BR102020022030A2 (en)
BR112023011738A2 (en)
BR112023016292A2 (en)
BR112023004146A2 (en)
BR112023011610A2 (en)
BR112023011539A2 (en)
BR112023008976A2 (en)
BR102021017576A2 (en)
BR102021015450A8 (en)
BR102021015220A2 (en)
BR102021015247A2 (en)
BR102021014044A2 (en)
BR102021013929A2 (en)
BR112021017747A2 (en)
BR102021012571A2 (en)
BR102021012230A2 (en)

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20220509

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20221213

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20230111

R150 Certificate of patent or registration of utility model

Ref document number: 7210805

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150